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Boeing 737 · Diff: NG 题库（47 题）

Boeing 737 机型「Diff: NG」相关知识共 47 道题。想练习或模拟考试，请到 题库 · 模拟考试。
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1.The maximum speed with the MACH TRIM system inoperative (737NG) is?

  1. 250/0.74M
  2. 280/0.80M
  3. 280/0.82M ✓
正确答案：280/0.82M　·　737　·　来源 b737.org.uk

2.The 737NG recommended turbulent penetration airspeed is

  1. 280Kts/0.72M
  2. 280Kts/0.76M ✓
  3. 280Kts/0.78M
正确答案：280Kts/0.76M　·　737　·　来源 b737.org.uk

3.The maximum landing weight of the B737-800 is

  1. 58,604-60,781 Kg
  2. 65,317-66,361 Kg ✓
  3. 65,361-71,350 Kg
正确答案：65,317-66,361 Kg　·　737　·　来源 b737.org.uk

4.The 737NG maximum differential pressure is

  1. 7.8 psi
  2. 8.35 psi
  3. 9.1 psi ✓
正确答案：9.1 psi　·　737　·　来源 b737.org.uk

5.The Allied Signal 131 APU maximum EGT is

  1. 760C
  2. Indicated by a red line on the EGT indicator.
  3. No limit ✓
正确答案：No limit　·　737　·　来源 b737.org.uk

6.The maximum aircraft altitude for electrical use of the Allied Signal 131 APU is

  1. 35,000ft
  2. 37,000ft.
  3. 41,000ft. ✓
正确答案：41,000ft.　·　737　·　来源 b737.org.uk

7.The 737NG Maximum N1 RPM is

  1. 105%.
  2. 106%.
  3. Indicated by a red line on the DU. ✓
正确答案：Indicated by a red line on the DU.　·　737　·　来源 b737.org.uk

8.The typical 737NG maximum fuel tank quantities are

  1. 4,600 kgs in each wing tank, 7,000 kgs in the centre tank
  2. 3,900 kgs in each wing tank, 12,800 kgs in the centre tank ✓
  3. 3,900 kgs in each wing tank, 16,200 kgs in the centre tank
正确答案：3,900 kgs in each wing tank, 12,800 kgs in the centre tank　·　737　·　来源 b737.org.uk

9.What is the approximate minimum engine oil quantity (per engine) for despatch on the 737NG.

  1. 12 US Quarts ie 69% Full ✓
  2. 12 US Quarts ie 75% Full
  3. 12 US Quarts ie 88% Full
正确答案：12 US Quarts ie 69% Full　·　737　·　来源 b737.org.uk

10.For a 737NG the automatic landing the head and crosswind limits are

  1. Headwind limit is 25 kts and the crosswind limit is 15 kts.
  2. Headwind limit is 20 kts and the crosswind limit is 15 kts.
  3. Headwind limit is 25 kts and the crosswind limit is 20 kts. ✓
正确答案：Headwind limit is 25 kts and the crosswind limit is 20 kts.　·　737　·　来源 b737.org.uk

11.The maximum demonstrated 737NG crosswind component for take-off and landing is

  1. 25 kts.
  2. 35 kts.
  3. 36 kts. ✓
正确答案：36 kts.　·　737　·　来源 b737.org.uk

12.The Allied Signal APU is rated at

  1. 80KVA up to FL310 and 45KVA above FL310.
  2. 90KVA up to FL310 and 55KVA above FL310.
  3. 90KVA up to FL310 and 66KVA above FL310. ✓
正确答案：90KVA up to FL310 and 66KVA above FL310.　·　737　·　来源 b737.org.uk

13.The 737NG fuel LOW indication

  1. Is amber and illuminates when the related main tank contains less than 907Kgs. ✓
  2. Is amber and illuminates when any main tank contains less than 907Kgs.
  3. Is amber and illuminates when the related main tank contains less than 1134Kgs.
正确答案：Is amber and illuminates when the related main tank contains less than 907Kgs.　·　737　·　来源 b737.org.uk

14.The 737NG fuel IMBAL indication

  1. Illuminates if the main tanks differ by more than 453kgs and will continue to display until imbalance is reduced to 91Kgs. ✓
  2. Illuminates if the main tanks differ by more than 453kgs and will continue to display until imbalance is reduced to 363Kgs.
  3. Illuminates if the main tanks differ by more than 453kgs and will continue to display until the crossfeed valve is opened.
正确答案：Illuminates if the main tanks differ by more than 453kgs and will continue to display until imbalance is reduced to 91Kgs.　·　737　·　来源 b737.org.uk

15.The 737NG fuel CONFIG indication illuminates if the center tank contains more than 726kgs, both centre tank pumps are producing low or no pressure and either engine is running...

  1. And will continue to display until centre tank is less than 91Kgs, one centre tank pump is producing high pressure or both engines are not running.
  2. And will continue to display until centre tank is less than 363Kgs, one centre tank pump is producing high pressure or both engines are not running. ✓
  3. And will continue to display until centre tank is less than 453Kgs, one centre tank pump is producing high pressure or both engines are not running.
正确答案：And will continue to display until centre tank is less than 363Kgs, one centre tank pump is producing high pressure or both engines are not running.　·　737　·　来源 b737.org.uk

16.737NG Centre tank fuel

  1. Is pressure fed ✓
  2. Is suction fed
  3. Is gravity fed
正确答案：Is pressure fed　·　737　·　来源 b737.org.uk

17.The 737NG centre tank fuel scavenge jet pump

  1. Is activated by a float switch ✓
  2. Is activated by the centre tank pump switches
  3. Is always active
正确答案：Is activated by a float switch　·　737　·　来源 b737.org.uk

18.Pulling an engine fire switch on the 737NG

  1. Closes both fuel valves. ✓
  2. Closes the spar fuel valve
  3. Closes the engine fuel valve
正确答案：Closes both fuel valves.　·　737　·　来源 b737.org.uk

19.The 737NG DISPLAYS CONTROL PANEL annunciation is accompanied by

  1. An ALT flag against the altitude tape. ✓
  2. A SPD flag against the speed tape.
  3. A V/S flag against the vertical speed tape.
正确答案：An ALT flag against the altitude tape.　·　737　·　来源 b737.org.uk

20.The 737NG hydraulic quantity RF annunciation displays when the hydraulic quantity is less than

  1. 69%
  2. 76% ✓
  3. 88%
正确答案：76%　·　737　·　来源 b737.org.uk

21.The 737NG overboard exhaust valve

  1. Is driven open if either pack switch is in HIGH and the recirc fan is OFF. ✓
  2. Is driven closed if either pack switch is in HIGH and the recirc fan is OFF.
  3. Is normally open in flight.
正确答案：Is driven open if either pack switch is in HIGH and the recirc fan is OFF.　·　737　·　来源 b737.org.uk

22.The 737NG antiskid switch

  1. Is not fitted to the NG. ✓
  2. Is guarded in the ON position.
  3. Is switched OFF for a manual reversion landing.
正确答案：Is not fitted to the NG.　·　737　·　来源 b737.org.uk

23.How many tyre damage impact fittings are there on the 737NG?

  1. One.
  2. Two. (One each side of the wheel well). ✓
  3. Four. (Two each side of each tyre recess).
正确答案：Two. (One each side of the wheel well).　·　737　·　来源 b737.org.uk

24.737NG Landing autobrake settings may be selected

  1. In-flight only.
  2. After touchdown prior to 60Kts. ✓
  3. After touchdown prior to 90Kts.
正确答案：After touchdown prior to 60Kts.　·　737　·　来源 b737.org.uk

25.The 737NG EEC gives redline protection for

  1. N1 and N2. ✓
  2. N1, N2 and EGT.
  3. N1, N2 and 5 minute limit.
正确答案：N1 and N2.　·　737　·　来源 b737.org.uk

26.The 737NG EEC will close the engine fuel shut off valve and de-energise the igniters during an engine start if:

  1. No increase in EGT within 15 seconds after the start lever is raised to IDLE. ✓
  2. EGT rapidly approaching the start limit.
  3. No increase in, or a very slow increase in N1 or N2 after EGT indication.
正确答案：No increase in EGT within 15 seconds after the start lever is raised to IDLE.　·　737　·　来源 b737.org.uk

27.The 737NG START VALVE OPEN, LOW OIL PRESSURE and OIL FILTER BYPASS lights

  1. Will blink for 10 seconds if condition occurs.
  2. Will blink for 10 seconds if condition occurs, except during take-off and landing. ✓
  3. Illuminate steady.
正确答案：Will blink for 10 seconds if condition occurs, except during take-off and landing.　·　737　·　来源 b737.org.uk

28.737NG: With flap 15 selected and landing gear UP, the landing gear warning horn cannot be silenced with the HORN CUTOUT switch if

  1. Both thrust levers are below approx 30 degrees.
  2. Either thrust lever is below 10 degrees or an engine not running and the other thrust lever is less than 30 degrees.
  3. Either thrust lever is below 20 degrees or an engine not running and the other thrust lever is less than 34 degrees. ✓
正确答案：Either thrust lever is below 20 degrees or an engine not running and the other thrust lever is less than 34 degrees.　·　737　·　来源 b737.org.uk

29.The 737NG Proximity Switch Electronic Unit (PSEU) light illuminates

  1. If an overwing exit flight lock fails to disengage when commanded at any time.
  2. If a fault is detected in the PSEU at any time.
  3. Is inhibited from thrust lever advance for take-off until 30 seconds after landing. ✓
正确答案：Is inhibited from thrust lever advance for take-off until 30 seconds after landing.　·　737　·　来源 b737.org.uk

30.737NG EGPWS terrain display changes from dotted to solid yellow

  1. 40 - 60 seconds from impact. ✓
  2. 20 - 30 seconds from impact.
  3. 30 - 60 seconds from impact.
正确答案：40 - 60 seconds from impact.　·　737　·　来源 b737.org.uk

31.The 737NG weather radar automatically begins scanning for windshear when:

  1. In flight below 2300ft RA. ✓
  2. In flight below 1200ft RA.
  3. In flight below 2500ft RA.
正确答案：In flight below 2300ft RA.　·　737　·　来源 b737.org.uk

32.737NG with FMC U10, after TOGA is pressed for a go-around, the CRZ page will show.

  1. The highest of: 1500ft or MCP altitude or the LEGS missed approach level. ✓
  2. The MCP altitude.
  3. The LEGS missed approach level.
正确答案：The highest of: 1500ft or MCP altitude or the LEGS missed approach level.　·　737　·　来源 b737.org.uk

33.The flap limit speed for a 737-800 FLAP 30 is

  1. 165Kts
  2. 175Kts ✓
  3. 185Kts
正确答案：175Kts　·　737　·　来源 b737.org.uk

34.The 737NG flap limit speed for FLAP 1 is

  1. 250K ✓
  2. 240K
  3. 230K
正确答案：250K　·　737　·　来源 b737.org.uk

35.The 737NG standby yaw damper is powered

  1. From the standby hydraulic system, only when both FLT CONTROL switches are positioned to STBY RUD. ✓
  2. From the standby hydraulic system, automatically when loss of system B hydraulic pressure is detected.
  3. From the standby hydraulic system, automatically when loss of system A and B hydraulic pressure is detected.
正确答案：From the standby hydraulic system, only when both FLT CONTROL switches are positioned to STBY RUD.　·　737　·　来源 b737.org.uk

36.The 737NG Flaps/Slat Electronics Unit (FSEU)

  1. Monitors flap load, assymetry, skew and overrun on all T/E flaps and L/E slats 2 to 7. ✓
  2. Monitors flap load, assymetry, skew and overrun on all T/E flaps and L/E slats.
  3. Monitors flap load, assymetry, skew and overrun on all T/E flaps and L/E slats and flaps.
正确答案：Monitors flap load, assymetry, skew and overrun on all T/E flaps and L/E slats 2 to 7.　·　737　·　来源 b737.org.uk

37.737NG: A leak in the system B hydraulic will also reduce the quantity in the B system

  1. To 20%
  2. To approx zero and is sufficient for PTU operation. ✓
  3. To approx 11% and is sufficient for PTU operation.
正确答案：To approx zero and is sufficient for PTU operation.　·　737　·　来源 b737.org.uk

38.The 737NG 'B' system reservoir has

  1. One standpipe. ✓
  2. Two standpipes.
  3. One standpipe used for reservoir pressurisation of the standby reservoir.
正确答案：One standpipe.　·　737　·　来源 b737.org.uk

39.737NG: A leak in the standby hydraulic system will also reduce the quantity in the B system to

  1. 64%
  2. 72% ✓
  3. 20%
正确答案：72%　·　737　·　来源 b737.org.uk

40.737NG: An IDG will auto disconnect due to

  1. Low oil pressure
  2. High oil temperature ✓
  3. Low oil quantity
正确答案：High oil temperature　·　737　·　来源 b737.org.uk

41.737NG TR UNIT light in-flight indicates

  1. Any TR has failed.
  2. TR1 or TR2 and TR3 failed. ✓
  3. TR1 and TR2 or TR3 failed
正确答案：TR1 or TR2 and TR3 failed.　·　737　·　来源 b737.org.uk

42.737NG: ELEC light means

  1. A fault exists in DC power system or standby power system.
  2. A fault exists in DC power system or standby power system and only operates on the ground. ✓
  3. A fault exists in DC power system, standby power system and only operates in-flight.
正确答案：A fault exists in DC power system or standby power system and only operates on the ground.　·　737　·　来源 b737.org.uk

43.737NG: The SOURCE OFF lights indicate that

  1. No source has been manually selected to power the related transfer bus, or the manually selected source has been disconnected. ✓
  2. No source has been manually selected to power the related transfer bus.
  3. No source has been manually selected to power the related transfer bus, or a source has been selected to power the opposite transfer bus.
正确答案：No source has been manually selected to power the related transfer bus, or the manually selected source has been disconnected.　·　737　·　来源 b737.org.uk

44.737NG: The STANDBY POWER OFF light illuminates if there is no power to either

  1. AC standby bus, DC standby bus or battery bus. ✓
  2. AC standby bus or battery bus.
  3. AC standby bus, DC standby bus or any of the battery buses.
正确答案：AC standby bus, DC standby bus or battery bus.　·　737　·　来源 b737.org.uk

45.On the 737 NG, The APU can power both Generator Busses

  1. On the ground only.
  2. In flight only.
  3. On the ground or in flight. ✓
正确答案：On the ground or in flight.　·　737　·　来源 b737.org.uk

46.On the 737 NG, If a landing is made with RTO left selected

  1. No automatic braking action occurs and the AUTOBRAKE DISARM light will illuminate two minutes after landing.
  2. No automatic braking action occurs and the AUTOBRAKE DISARM light will illuminate 2 seconds after landing. ✓
  3. Full automatic RTO braking occurs and the AUTOBRAKE DISARM light would not illuminate.
正确答案：No automatic braking action occurs and the AUTOBRAKE DISARM light will illuminate 2 seconds after landing.　·　737　·　来源 b737.org.uk

47.The minimum fuel temperature prior to take-off and in-flight for the CL is - 45°C, or 3°C above the fuel freezing point temperature, whichever is higher. What is it for the 737NG/MAX?

  1. - 43°C, or 3°C above the fuel freezing point temperature, whichever is higher. ✓
  2. - 47°C, or 3°C above the fuel freezing point temperature, whichever is higher.
  3. - 49°C, or 3°C above the fuel freezing point temperature, whichever is higher.
正确答案：- 43°C, or 3°C above the fuel freezing point temperature, whichever is higher.　·　737　·　来源 b737.org.uk
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